View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 64490U 26145.21456034 +.00000000 +00000-0 +14580-2 0 00009
2 64490 53.1568 121.4187 0000831 91.0562 269.0534 15.30248036 03
| Epoch (UTC): | 25 May 2026 05:08:58 |
| Eccentricity: | 0.0000831 |
| inclination: | 53.1568° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 121.4187° |
| argument of perigee: | 91.0562° |
| revolutions per day: | 15.30248036 |
| mean anomaly at epoch: | 269.0534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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